WEKO3
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月軟着陸技術の研究:月着陸航法誘導技術の研究
https://jaxa.repo.nii.ac.jp/records/2689
https://jaxa.repo.nii.ac.jp/records/2689e02a80d2-9e41-4991-9862-a8b4c4f7e943
名前 / ファイル | ライセンス | アクション |
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48129025.pdf (693.4 kB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 月軟着陸技術の研究:月着陸航法誘導技術の研究 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | SELENE-B | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 月探査 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 月面軟着陸 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 航法誘導 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高度計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | イメージセンサ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 障害物回避 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | シミュレーション | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | SELENE-B | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | lunar exploration | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | lunar soft landing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | navigation and guidance | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | altimeter | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | image sensor | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | obstacle avoidance | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | simulation | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Study on lunar soft landing: Study on guidance and navigation for lunar landing | |||||
著者 |
山本, 昌幸
× 山本, 昌幸× 石島, 義之× 濱田, 吉郎× 二宮, 哲次郎× 松本, 甲太郎× 四宮, 康雄× 澤井, 秀次郎× 橋本, 樹明× 神谷, 芳和× Yamamoto, Masayuki× Ishijima, Yoshiyuki× Hamada, Yoshiro× Ninomiya, Tetsujiro× Matsumoto, Kotaro× Shinomiya, Yasuo× Sawai, Shujiro× Hashimoto, Tatsuaki× Kamiya, Yoshikazu |
|||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構研究開発資料: 平成15年度総合技術研究本部宇宙領域研究成果報告書:先行研究等 en : JAXA Research and Development Memorandum: FY15 Annual Report of Research & Development on Space Technology in the Institute of Space Technology and Aeronautics: Advanced Technology 巻 JAXA-RM-04-011, p. 123-128, 発行日 2004-10-29 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In order to realize the science missions at the specific point on the moon, SELENE-B is required highly precise and safe landing. This paper shows the result of the guidance and navigation simulation and estimates the landing accuracy. This simulation is combined the navigation law and guidance law. The navigation law is realized by using the image sensor and the altimeter. The guidance law is restricted using the ON/OFF control thruster. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-1121 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11983593 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0048129025 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-RM-04-011 |